EP0137470A2 - Intake system for internal combustion engine - Google Patents
Intake system for internal combustion engine Download PDFInfo
- Publication number
- EP0137470A2 EP0137470A2 EP84111962A EP84111962A EP0137470A2 EP 0137470 A2 EP0137470 A2 EP 0137470A2 EP 84111962 A EP84111962 A EP 84111962A EP 84111962 A EP84111962 A EP 84111962A EP 0137470 A2 EP0137470 A2 EP 0137470A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- throttle valve
- passage
- air
- downstream
- induction passage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M69/00—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
- F02M69/30—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for facilitating the starting-up or idling of engines or by means for enriching fuel charge, e.g. below operational temperatures or upon high power demand of engines
- F02M69/32—Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel characterised by means for facilitating the starting-up or idling of engines or by means for enriching fuel charge, e.g. below operational temperatures or upon high power demand of engines with an air by-pass around the air throttle valve or with an auxiliary air passage, e.g. with a variably controlled valve therein
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S261/00—Gas and liquid contact apparatus
- Y10S261/82—Upper end injectors
Definitions
- the present invention relates to an intake system for internal combustion engines and, more particularly, to an engine intake system of the type that employs a single or a plurality of fuel injectors disposed in an induction passage upstream of a throttle valve to inject jets of fuel into the induction passage.
- the present invention has an object to provide an intake system for an internal combustion engine which is improved to assure a stable engine idle operation.
- the intake system for an internal combustion engine comprises:
- Japanese Pre-Examination Patent Publication No. 79666/83 discloses an intake system for an internal combustion engine which system includes a single or a plurality of fuel injectors for injecting jets of fuel into an induction passage upstream of a throttle valve disposed therein.
- the throttle valve is rotatable about the axis of a throttle shaft between idle and fully opon positions.
- the throttle valve is inclined to the axis of the induction passage and has upstream and downstream edge portions slightly spaced from the inner peripheral surface of the induction passage to cooperate therewith to define narrow gaps through which air and the injected fuel particles are allowed to pass toward engine cylinders.
- the prior art intake system shown in Fig. 1 has a throttle valve 3 formed by a circular throttle plate mounted on a rotatable throttle shaft 3a extending diametrically through an induction passage 2 a part of which is defined in a throttle body 1.
- a fuel injector 4 is supported by a holder 4a disposed centrally of a venturi chamber 4b to cooperate therewith to define an annular venturi 9 which forms a part of the induction passage 2.
- a bypass air passage 7 is formed in the peripheral wall of the venturi chamber 4b and has an upstream end open to a part 8 of the induction passage situated upstream of the venturi 9. The downstream end of the bypass air passage 7 is open to the venturi 9.
- a conventional electric air flow meter 5 is attached to the outer peripheral surface of the venturi chamber 4b and includes a hot-wire type air flow sensor or temperature-sensitive resistor 5a disposed in the bypass air passage 7 to meter the flow of air therethrough and thus to determine the total air flow through the induction passage into an associated engine (not shown).
- the air flow meter 5 produces an electric signal representive of the rate of air flow into the engine and emits the signal to a computor 6 which is operative in response to the input signal to compute the rate of fuel supply optimum to the rate of air supply to the engine for thereby emitting fuel supply signals to the injector 4.
- the injector 4 is responsive to the fuel supply signals from the computor 6 to inject jets of liquid fuel into the induction passage 2 so that the engine is supplied with a mixture of air and fuel at an air/fuel ratio most suited to the engine operation.
- liquid mass When the liquid mass has grown to a certain size, a part of the liquid fuel is separated from the mass to form drops 11 which are then fed into the engine.
- the formation of the liquid mass is quire undesirable to engine idle operations because the addition of the fuel drops 11 to continuous supply of normal air-fuel mixture to the engine is discontinuous and causes a non-uniform rate of fuel supply during an engine idle operation, resulting in an unstable idle operation of the engine, and because the introduction of the liquid fuel drops into the engine increases the CO and HC contents of the engine exhaust gases.
- the improvement of the embodiment of the present invention shown in Figs. 2 and 3 comprises an air passage 12 formed in the peripheral wall of the throttle body 1 and extends in bypassing relationship to the gap 10 defined between the inner peripheral surface of the throttle body 1 and the upward edge portion of the throttle valve 3 when it is in its idle position.
- the bypass air passage 12 has its upstream end 13 open to the induction passage 2 at a point disposed radially outwardly of the cone of the jet of fuel injected by the fuel injector 4.
- the downstream end 15 of the bypass air passage 12 is open to the induction passage 2 at a point downstream of the upstream edge portion of the throttle valve 3 when in its idle position and directed substantially toward the central zone of the undersurface or downstream face of the throttle valve 3.
- bypass air passage 12 When the engine is in its idle operation, a part of the air which has passed through the venturi 9 enters the bypass air passage 12 and flows therethrough in bypassing relationship to the flow of air and fuel particles passing through the gap 10.
- the bypass air is then jetted through the downstream end 15 of the bypass air passage 12 into the induction passage 2 downstream of the throttle valve 3.
- the jet of air is directed substantially toward the central zone of the downstream face of the throttle valve 3 to eliminate or compensate for the difference in pressure between the induction passage 2 just downstream of the throttle valve 3 and the sections of the induction passage 2 adjacent to the gaps 10 which difference would otherwise be caused due to the reason discussed above in'connection with the prior art.
- the upstream end 13 of the bypass air passage 12 is disposed outwardly of the cone of the jet of fuel injected by the injector 4, the air flowing through the bypass air passage 12 and jetted through the downstream end 15 thereof does not contain any amount of fuel.
- the inner peripheral surface of the induction passage 2 downstream of the downstream end 15 of the bypass air passage 12 is prevented from being adhered by any liquid film or drops of the fuel which would oterwise flow through the bypass air passage 12.
- Such a liquid film or drops of fuel cannot easily be atomized and thus will adversely affect the engine operation and emission control.
- the upstream end 13 of the bypass air passage 12 is located downstream of the downstream end 14 of the first bypass air passage 7 which contains the temperature-sensitive air flow sensor element 5a.
- the part of the air flow which passes through the second bypass air passage 12 is included in the total air flow to the engine which has already been measured by the air flow meter 5. This feature is advantageous in the view point of air-fuel ratio control.
- the position of the downstream end 15 of the bypass air passage 12 is important to attain the intended purpose.
- the downstream end 15 is positioned at a level substantially the same as the level of the downstream edge portion of the throttle valve 3 when in its idle position.
- the downstream end 15 of the bypass air passage 12 is located. immediately or slightly below the upstream edge portion of the throttle valve 3 when in the idle position.
- the bypass air passage downstream end 15, however, is not limited to the positions shown in Figs. 2 and 4 and can be located at any point within the distance or range defined between the positions shown in Figs. 2 and 4.
- bypass air passage downstream end 15 should be open in the induction passage 2 on the side thereof substantially aligned with the upstream edge portion of the throttle valve 3 as viewed in the flow of air through the induction passage 2, namely, on the righthand side of the induction passage 2 as viewed on the illustrations in Figs. 2 and 4. If the downstream end 15 of the bypass air passage 12 were formed in the lefthand side of the induction passage 2, i.e., adjacent to the downstream edge portion of the throttle valve 3, the air jetted from such a downstream end will not be operative to prevent the downsteram face of the throttle valve 3 from being adhered by fuel particles.
- the downsteam end 15 of the bypass air passage 12 is in the form of a circular opening 15A, as shown in Fig. 3.
- the bypass air passage downstream end 15 is in the form of an arcuate slit or groove 15B formed in the inner peripheral surface of the throttle body 1 and extending circumferentially thereof over a predetermined angle.
- the opposite ends of the length of the groove 15B are shaped to direct air substantially toward the central area of the undersurface or downstream face of the throttle valve 3 when it is in its idle position.
- an air nozzle 17 is fitted into the downstream end of the bypass air passage 12 and extends inwardly from the inner peripheral surface of the throttle body 1 substantially toward the center of the bypass air passage 2.
- the air nozzle 17 is provided with nozzle orifice 17A adjacent to the inner end of the nozzle 17.
- the air entering the bypass air passage 12 is jetted through the nozzle orifice 17A to the central space of the induction passage just downstream of the throttle valve to reliably compensate for the diference in pressure between the central space of the induction passage immediately downstream of the throttle valve 3 and the peripheral zone of the induction passage 2 adjacent to the gaps 10, whereby the whirling-up of the air and fuel particles just downstream of the throttle valve is prevented.
- the nozzle orifice 17A adjacent to the inner end of the air nozzle 17 defines the narrowest section of the bypass air passage 12, so that the air is jetted through the nozzle orifice 17A substantially at sonic velocity.
- the sonic air jet therefore, is operative to atomize the fuel particles in the induction passage just downstream of the throttle valve to thereby improve the stability of the engine idle operation.
- the intake system according to the present invention is effete to prevent the formation of drops of fuel during engine idle operations for thereby ensuring smooth engine idle operations and reduced emissin of CO and HC during engine idle operations.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Description
- The present invention relates to an intake system for internal combustion engines and, more particularly, to an engine intake system of the type that employs a single or a plurality of fuel injectors disposed in an induction passage upstream of a throttle valve to inject jets of fuel into the induction passage.
- The present invention has an object to provide an intake system for an internal combustion engine which is improved to assure a stable engine idle operation.
- The intake system for an internal combustion engine according to the present invention comprises:
- means defining an induction passage;
- a throttle valve disposed in the induction passage;
- at least one injector disposed in the induction passage upstream of the throttle valve and so arranged as to inject a jet of fuel therein;
- the throttle valve being movable between idle and wide-open positions, the throttle valve when in the idle position having an edge portion slightly spaced from the inner peripheral surface of the induction passage to define therewith a narrow gap for the passage of air and fuel for an engine idle operation; and
- means defining an air passage extending in bypassing relationship to the narrow gap and terminating in a downstream air outlet end arranged to direct a jet of bypassing air substantially toward a central space immediately downstream of the throttle valve when in the idle position.
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- Fig. 1 is an axial sectional view of the prior art intake system;
- Fig. 2 is a similar view but shows an embodiment of the intake system for an internal combustin engine according to the present invention;
- Fig. 3 is a cross-section taken along line III - III in Fig. 2;
- Fig. 4 is similar to Fig. 2 but illustrates a modification to the embodiment shown in Fig. 2;
- Fig. 5 shows a modification to the embodiment shown in Fig. 3; and
- Fig. 6 is similar to Figs. 2 and 4 but illustrates another embodiment of the invention.
- Japanese Pre-Examination Patent Publication No. 79666/83 discloses an intake system for an internal combustion engine which system includes a single or a plurality of fuel injectors for injecting jets of fuel into an induction passage upstream of a throttle valve disposed therein. The throttle valve is rotatable about the axis of a throttle shaft between idle and fully opon positions. When the engine is in its idle operation, the throttle valve is inclined to the axis of the induction passage and has upstream and downstream edge portions slightly spaced from the inner peripheral surface of the induction passage to cooperate therewith to define narrow gaps through which air and the injected fuel particles are allowed to pass toward engine cylinders. A part of the air and fuel particles then whirls toward the center of the underside of the throttle valve due to vacuum immediately downstream of the throttle valve whereby vortices are generated downstream of the throttle valve. The fuel particles suspended in the whirling air streams tend to be gathered at a central zone of the vortices to form a mass of liquid fuel. When the liquid mass has grown to a certain size, a part of the liquid mass is separated therefrom to form drops which are sucked into the engine. For this reason, the fuel is not fed into the engine at a uniform rate all over an idle operation, resulting in unstable engine idle operations and difficulties in the emission control, as will be discussed in more detail hereunder with reference to Fig. 1 which shows a typical one point fuel injection type intake system of the prior art.
- The prior art intake system shown in Fig. 1 has a
throttle valve 3 formed by a circular throttle plate mounted on a rotatable throttle shaft 3a extending diametrically through an induction passage 2 a part of which is defined in a throttle body 1. Afuel injector 4 is supported by aholder 4a disposed centrally of aventuri chamber 4b to cooperate therewith to define anannular venturi 9 which forms a part of theinduction passage 2. Abypass air passage 7 is formed in the peripheral wall of theventuri chamber 4b and has an upstream end open to apart 8 of the induction passage situated upstream of theventuri 9. The downstream end of thebypass air passage 7 is open to theventuri 9. - A conventional electric
air flow meter 5 is attached to the outer peripheral surface of theventuri chamber 4b and includes a hot-wire type air flow sensor or temperature-sensitive resistor 5a disposed in thebypass air passage 7 to meter the flow of air therethrough and thus to determine the total air flow through the induction passage into an associated engine (not shown). Theair flow meter 5 produces an electric signal representive of the rate of air flow into the engine and emits the signal to acomputor 6 which is operative in response to the input signal to compute the rate of fuel supply optimum to the rate of air supply to the engine for thereby emitting fuel supply signals to theinjector 4. Theinjector 4 is responsive to the fuel supply signals from thecomputor 6 to inject jets of liquid fuel into theinduction passage 2 so that the engine is supplied with a mixture of air and fuel at an air/fuel ratio most suited to the engine operation. - In the intake system of the type described above, when the
throttle plate 3 is in its idle position shown in Fig. 1, the air and the fuel particles passing throughnarrow gaps 10 defined between the upper (upstream) and lower (downstream) edge portions of thethrottle plate 3 are whirled toward the central zone of theinduction passage 2 immediately below the throttle shaft and downstream of thethrottle plate 3, as schematically illustrated in Fig. 1. This is because of the difference in pressure between the sections of theinduction passage 2 adjacent to thenarrow gaps 10 and the central section of the induction passage just downstream of thethrottle plate 3. The whirled air streams and fuel particles are gathered to a central space of the induction passage just downstream of thethrottle valve 3. The fuel particles thus gathered form a mass of liquid fluid. When the liquid mass has grown to a certain size, a part of the liquid fuel is separated from the mass to form drops 11 which are then fed into the engine. The formation of the liquid mass is quire undesirable to engine idle operations because the addition of the fuel drops 11 to continuous supply of normal air-fuel mixture to the engine is discontinuous and causes a non-uniform rate of fuel supply during an engine idle operation, resulting in an unstable idle operation of the engine, and because the introduction of the liquid fuel drops into the engine increases the CO and HC contents of the engine exhaust gases. - Preferred embodiments of the invention will now be described with reference to Figs. 2 to 6 of the drawings wherein the parts and elements the same as in the prior art shown in Fig. 1 are designated by the same reference numerals. Only the improvement of the invention over the described prior art will be described hereunder for the purpose of simplifying the description.
- The improvement of the embodiment of the present invention shown in Figs. 2 and 3 comprises an
air passage 12 formed in the peripheral wall of the throttle body 1 and extends in bypassing relationship to thegap 10 defined between the inner peripheral surface of the throttle body 1 and the upward edge portion of thethrottle valve 3 when it is in its idle position. Thebypass air passage 12 has itsupstream end 13 open to theinduction passage 2 at a point disposed radially outwardly of the cone of the jet of fuel injected by thefuel injector 4. In the illustrated embodiment of the invention, thedownstream end 15 of thebypass air passage 12 is open to theinduction passage 2 at a point downstream of the upstream edge portion of thethrottle valve 3 when in its idle position and directed substantially toward the central zone of the undersurface or downstream face of thethrottle valve 3. - Thus, when the engine is in its idle operation, a part of the air which has passed through the
venturi 9 enters thebypass air passage 12 and flows therethrough in bypassing relationship to the flow of air and fuel particles passing through thegap 10. The bypass air is then jetted through thedownstream end 15 of thebypass air passage 12 into theinduction passage 2 downstream of thethrottle valve 3. The jet of air is directed substantially toward the central zone of the downstream face of thethrottle valve 3 to eliminate or compensate for the difference in pressure between theinduction passage 2 just downstream of thethrottle valve 3 and the sections of theinduction passage 2 adjacent to thegaps 10 which difference would otherwise be caused due to the reason discussed above in'connection with the prior art. Accordingly, the air and fuel particles which have passed through thegaps 10 flow smoothly toward the engine and will not be whirled up to the center of theinduction passage 2 immediately downstream of the throttle valve. For this reason, the production of a liquid mass and resultant formation of fuel drops, which have taken place in the prior art, are advantageously avoided to assure a stable fuel supply to the engine at a substantially constant rate all over an engine idle operation for thereby insuring a stable engine idle operation and minimized emission of CO and HC. - It will be appreciated that, because the
upstream end 13 of thebypass air passage 12 is disposed outwardly of the cone of the jet of fuel injected by theinjector 4, the air flowing through thebypass air passage 12 and jetted through thedownstream end 15 thereof does not contain any amount of fuel. Thus, the inner peripheral surface of theinduction passage 2 downstream of thedownstream end 15 of thebypass air passage 12 is prevented from being adhered by any liquid film or drops of the fuel which would oterwise flow through thebypass air passage 12. Such a liquid film or drops of fuel cannot easily be atomized and thus will adversely affect the engine operation and emission control. - In addition, the
upstream end 13 of thebypass air passage 12 is located downstream of thedownstream end 14 of the firstbypass air passage 7 which contains the temperature-sensitive airflow sensor element 5a. Thus, the part of the air flow which passes through the secondbypass air passage 12 is included in the total air flow to the engine which has already been measured by theair flow meter 5. This feature is advantageous in the view point of air-fuel ratio control. - The position of the
downstream end 15 of thebypass air passage 12 is important to attain the intended purpose. In the embodiment of the invention shown in Fig. 2, thedownstream end 15 is positioned at a level substantially the same as the level of the downstream edge portion of thethrottle valve 3 when in its idle position. However, in the modification shown in Fig. 4, thedownstream end 15 of thebypass air passage 12 is located. immediately or slightly below the upstream edge portion of thethrottle valve 3 when in the idle position. The bypass air passage downstreamend 15, however, is not limited to the positions shown in Figs. 2 and 4 and can be located at any point within the distance or range defined between the positions shown in Figs. 2 and 4. - Secondly, the bypass air passage downstream
end 15 should be open in theinduction passage 2 on the side thereof substantially aligned with the upstream edge portion of thethrottle valve 3 as viewed in the flow of air through theinduction passage 2, namely, on the righthand side of theinduction passage 2 as viewed on the illustrations in Figs. 2 and 4. If thedownstream end 15 of thebypass air passage 12 were formed in the lefthand side of theinduction passage 2, i.e., adjacent to the downstream edge portion of thethrottle valve 3, the air jetted from such a downstream end will not be operative to prevent the downsteram face of thethrottle valve 3 from being adhered by fuel particles. - In the embodiment of the invention shown in Fig. 2 and the modification shown in Fig. 4, the
downsteam end 15 of thebypass air passage 12 is in the form of acircular opening 15A, as shown in Fig. 3. In the modification shown in Fig. 5, however, the bypass air passage downstreamend 15 is in the form of an arcuate slit orgroove 15B formed in the inner peripheral surface of the throttle body 1 and extending circumferentially thereof over a predetermined angle. The opposite ends of the length of thegroove 15B are shaped to direct air substantially toward the central area of the undersurface or downstream face of thethrottle valve 3 when it is in its idle position. - When the
throttle valve 3 is in a wide-open position, the pressure in theinduction passage 2 downstream of the throttle valve is substantially equal to the pressure in theinduction passage 2 upstream of thethrottle valve 3. In such an engine operating condition, therefore, little air flows through thebypass air passage 12. Thus, the flow of air through thebypass air passage 12 takes place only when the pressure differential across thethrottle valve 3 exceeds a predetermined level. - In the second embodiment shown in Fig. 6 of the drawings, an
air nozzle 17 is fitted into the downstream end of thebypass air passage 12 and extends inwardly from the inner peripheral surface of the throttle body 1 substantially toward the center of thebypass air passage 2. Theair nozzle 17 is provided withnozzle orifice 17A adjacent to the inner end of thenozzle 17. The air entering thebypass air passage 12 is jetted through thenozzle orifice 17A to the central space of the induction passage just downstream of the throttle valve to reliably compensate for the diference in pressure between the central space of the induction passage immediately downstream of thethrottle valve 3 and the peripheral zone of theinduction passage 2 adjacent to thegaps 10, whereby the whirling-up of the air and fuel particles just downstream of the throttle valve is prevented. Thenozzle orifice 17A adjacent to the inner end of theair nozzle 17 defines the narrowest section of thebypass air passage 12, so that the air is jetted through thenozzle orifice 17A substantially at sonic velocity. The sonic air jet, therefore, is operative to atomize the fuel particles in the induction passage just downstream of the throttle valve to thereby improve the stability of the engine idle operation. - As described above, the intake system according to the present invention is efective to prevent the formation of drops of fuel during engine idle operations for thereby ensuring smooth engine idle operations and reduced emissin of CO and HC during engine idle operations.
Claims (10)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP187043/83 | 1983-10-07 | ||
JP58187043A JPS6079162A (en) | 1983-10-07 | 1983-10-07 | Fuel injector |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0137470A2 true EP0137470A2 (en) | 1985-04-17 |
EP0137470A3 EP0137470A3 (en) | 1987-04-01 |
EP0137470B1 EP0137470B1 (en) | 1989-08-02 |
Family
ID=16199171
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP84111962A Expired EP0137470B1 (en) | 1983-10-07 | 1984-10-05 | Intake system for internal combustion engine |
Country Status (6)
Country | Link |
---|---|
US (1) | US4584981A (en) |
EP (1) | EP0137470B1 (en) |
JP (1) | JPS6079162A (en) |
KR (1) | KR920002515B1 (en) |
CA (1) | CA1221590A (en) |
DE (1) | DE3479231D1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2204358A (en) * | 1987-04-30 | 1988-11-09 | Weber Srl | I.c. engine fuel injector throttle body |
US4926821A (en) * | 1985-11-02 | 1990-05-22 | Vdo Adolf Schindling Ag | Electronic controller for internal combustion engines |
GB2303405A (en) * | 1995-07-14 | 1997-02-19 | Nippon Denso Co | I.c. engine throttle valve apparatus with freeze prevention |
US5704335A (en) * | 1995-07-14 | 1998-01-06 | Nippondenso Co., Ltd. | Throttle valve apparatus for internal combustion engine |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6296776A (en) * | 1985-10-23 | 1987-05-06 | Nissan Motor Co Ltd | Fuel feeder for itnernal combustion engine |
JPH0612755U (en) * | 1992-07-21 | 1994-02-18 | 日本電装株式会社 | Mixture supply device for internal combustion engine |
US5575264A (en) * | 1995-12-22 | 1996-11-19 | Siemens Automotive Corporation | Using EEPROM technology in carrying performance data with a fuel injector |
US6467465B1 (en) * | 2001-01-10 | 2002-10-22 | Anthony R. Lorts | Throttle body fuel injector adapter manifold |
AU756938B1 (en) | 2002-04-04 | 2003-01-30 | Hyundai Motor Company | Engine idle speed control device |
US7007930B1 (en) * | 2003-11-24 | 2006-03-07 | Walbro Engine Management, L.L.C. | Dual fuel feed system carburetor |
US10082092B2 (en) | 2014-04-03 | 2018-09-25 | Ford Global Technologies, Llc | Method and system for vacuum generation using a throttle |
US9964080B2 (en) | 2016-08-25 | 2018-05-08 | Ford Global Technologies, Llc | Method and system for vacuum generation using a throttle |
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US2487774A (en) * | 1943-11-17 | 1949-11-08 | Pieter W Schipper | Fuel metering device |
US3814389A (en) * | 1972-05-02 | 1974-06-04 | P August | Carburetor |
FR2251717A1 (en) * | 1973-11-16 | 1975-06-13 | Ford France | |
GB2052796A (en) * | 1979-05-09 | 1981-01-28 | Hitachi Ltd | Automatic control of air/fuel ratio in i c engines |
DE3032066A1 (en) * | 1980-08-26 | 1982-04-15 | Robert Bosch Gmbh, 7000 Stuttgart | MIXING FORMATION SYSTEM FOR MIXTURING COMPRESSIVE IGNITION ENGINES |
DE3034996A1 (en) * | 1980-09-17 | 1982-04-29 | Hans Jürgen Bregenz August | Fuel injected IC engine - has additional air inlet jets near throttle to homogenise fuel air mixture |
US4359983A (en) * | 1981-04-02 | 1982-11-23 | General Motors Corporation | Engine idle air control valve with position counter reset apparatus |
JPS5879666A (en) * | 1981-10-16 | 1983-05-13 | ロ−ベルト・ボツシユ・ゲゼルシヤフト・ミツト・ベシユレンクテル・ハフツング | Fuel injector for internal combustion engine |
EP0088393A1 (en) * | 1982-03-04 | 1983-09-14 | Hitachi, Ltd. | Fuel controller for internal combustion engine |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS55156239A (en) * | 1979-05-24 | 1980-12-05 | Nippon Denso Co Ltd | Air intake device of engine |
JPS59165862A (en) * | 1983-03-08 | 1984-09-19 | Automob Antipollut & Saf Res Center | Single-point fuel injection device |
-
1983
- 1983-10-07 JP JP58187043A patent/JPS6079162A/en active Granted
-
1984
- 1984-10-04 CA CA000464734A patent/CA1221590A/en not_active Expired
- 1984-10-04 KR KR1019840006140A patent/KR920002515B1/en not_active IP Right Cessation
- 1984-10-05 DE DE8484111962T patent/DE3479231D1/en not_active Expired
- 1984-10-05 EP EP84111962A patent/EP0137470B1/en not_active Expired
- 1984-10-05 US US06/658,024 patent/US4584981A/en not_active Expired - Fee Related
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2487774A (en) * | 1943-11-17 | 1949-11-08 | Pieter W Schipper | Fuel metering device |
US3814389A (en) * | 1972-05-02 | 1974-06-04 | P August | Carburetor |
FR2251717A1 (en) * | 1973-11-16 | 1975-06-13 | Ford France | |
GB2052796A (en) * | 1979-05-09 | 1981-01-28 | Hitachi Ltd | Automatic control of air/fuel ratio in i c engines |
DE3032066A1 (en) * | 1980-08-26 | 1982-04-15 | Robert Bosch Gmbh, 7000 Stuttgart | MIXING FORMATION SYSTEM FOR MIXTURING COMPRESSIVE IGNITION ENGINES |
DE3034996A1 (en) * | 1980-09-17 | 1982-04-29 | Hans Jürgen Bregenz August | Fuel injected IC engine - has additional air inlet jets near throttle to homogenise fuel air mixture |
US4359983A (en) * | 1981-04-02 | 1982-11-23 | General Motors Corporation | Engine idle air control valve with position counter reset apparatus |
JPS5879666A (en) * | 1981-10-16 | 1983-05-13 | ロ−ベルト・ボツシユ・ゲゼルシヤフト・ミツト・ベシユレンクテル・ハフツング | Fuel injector for internal combustion engine |
EP0088393A1 (en) * | 1982-03-04 | 1983-09-14 | Hitachi, Ltd. | Fuel controller for internal combustion engine |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4926821A (en) * | 1985-11-02 | 1990-05-22 | Vdo Adolf Schindling Ag | Electronic controller for internal combustion engines |
GB2204358A (en) * | 1987-04-30 | 1988-11-09 | Weber Srl | I.c. engine fuel injector throttle body |
US4905651A (en) * | 1987-04-30 | 1990-03-06 | Weber S.R.L. | Device for forming and metering an air and fuel mixture for an internal combustion engine |
GB2204358B (en) * | 1987-04-30 | 1992-02-19 | Weber Srl | Device for forming and metering an air and fuel mixture for an internal combustion engine |
GB2303405A (en) * | 1995-07-14 | 1997-02-19 | Nippon Denso Co | I.c. engine throttle valve apparatus with freeze prevention |
US5704335A (en) * | 1995-07-14 | 1998-01-06 | Nippondenso Co., Ltd. | Throttle valve apparatus for internal combustion engine |
GB2303405B (en) * | 1995-07-14 | 1999-01-20 | Nippon Denso Co | Intake air controlling apparatus for an internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
EP0137470A3 (en) | 1987-04-01 |
US4584981A (en) | 1986-04-29 |
KR850003931A (en) | 1985-06-29 |
DE3479231D1 (en) | 1989-09-07 |
JPH0211734B2 (en) | 1990-03-15 |
JPS6079162A (en) | 1985-05-04 |
EP0137470B1 (en) | 1989-08-02 |
KR920002515B1 (en) | 1992-03-27 |
CA1221590A (en) | 1987-05-12 |
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